{"status":"ok","message-type":"work","message-version":"1.0.0","message":{"indexed":{"date-parts":[[2025,10,26]],"date-time":"2025-10-26T14:36:49Z","timestamp":1761489409984,"version":"3.28.0"},"reference-count":16,"publisher":"IEEE","content-domain":{"domain":[],"crossmark-restriction":false},"short-container-title":[],"published-print":{"date-parts":[[2012,6]]},"DOI":"10.1109\/acc.2012.6315426","type":"proceedings-article","created":{"date-parts":[[2014,7,16]],"date-time":"2014-07-16T21:55:22Z","timestamp":1405547722000},"page":"155-160","source":"Crossref","is-referenced-by-count":1,"title":["Characterizing the reachable set for a spacecraft with two rotors"],"prefix":"10.1109","author":[{"given":"R.","family":"Bayadi","sequence":"first","affiliation":[]},{"given":"R. N.","family":"Banavar","sequence":"additional","affiliation":[]},{"family":"Dong Eui Chang","sequence":"additional","affiliation":[]}],"member":"263","reference":[{"journal-title":"Topology Geometry and Gauge Fields Foundations","year":"2011","author":"naber","key":"15"},{"key":"16","doi-asserted-by":"publisher","DOI":"10.1109\/9.362852"},{"key":"13","doi-asserted-by":"publisher","DOI":"10.1017\/CBO9780511624001"},{"key":"14","doi-asserted-by":"publisher","DOI":"10.1080\/713603744"},{"key":"11","doi-asserted-by":"publisher","DOI":"10.1063\/1.533317"},{"key":"12","doi-asserted-by":"crossref","DOI":"10.1007\/978-0-387-21792-5","author":"marsden","year":"1999","journal-title":"Introduction to Mechanics and Symmetry"},{"key":"3","doi-asserted-by":"publisher","DOI":"10.1109\/CDC.1996.573511"},{"key":"2","doi-asserted-by":"publisher","DOI":"10.1016\/S0947-3580(96)70028-6"},{"key":"1","doi-asserted-by":"publisher","DOI":"10.1109\/TAC.1984.1103519"},{"key":"10","doi-asserted-by":"publisher","DOI":"10.2514\/1.21505"},{"key":"7","article-title":"Attitude control of an underactuated small satellite","author":"horri","year":"2003","journal-title":"Proceedings of IEEE Aerospace Conference"},{"key":"6","doi-asserted-by":"crossref","first-page":"256","DOI":"10.2514\/3.21378","article-title":"Attitude stabilization of a rigid spacecraft using two reaction wheel actuators","volume":"18","author":"krishnan","year":"1995","journal-title":"Journal of Guidance Control and Dynamics"},{"key":"5","doi-asserted-by":"publisher","DOI":"10.1109\/CDC.1997.657855"},{"key":"4","doi-asserted-by":"publisher","DOI":"10.2514\/2.4097"},{"key":"9","article-title":"Momentum transfer control of a spacecraft with two wheels by feedback linearization","author":"leeghim","year":"2008","journal-title":"Proceedings of International Conference on Control Automation and Systems"},{"key":"8","article-title":"Feedback attitude control of a spacecraft by two reaction wheels","author":"yamada","year":"1998","journal-title":"Proceedings of 21st International Symposium on Space Technology and Science"}],"event":{"name":"2012 American Control Conference - ACC 2012","start":{"date-parts":[[2012,6,27]]},"location":"Montreal, QC","end":{"date-parts":[[2012,6,29]]}},"container-title":["2012 American Control Conference (ACC)"],"original-title":[],"link":[{"URL":"http:\/\/xplorestaging.ieee.org\/ielx5\/6297579\/6314593\/06315426.pdf?arnumber=6315426","content-type":"unspecified","content-version":"vor","intended-application":"similarity-checking"}],"deposited":{"date-parts":[[2017,6,22]],"date-time":"2017-06-22T16:50:27Z","timestamp":1498150227000},"score":1,"resource":{"primary":{"URL":"http:\/\/ieeexplore.ieee.org\/document\/6315426\/"}},"subtitle":[],"short-title":[],"issued":{"date-parts":[[2012,6]]},"references-count":16,"URL":"https:\/\/doi.org\/10.1109\/acc.2012.6315426","relation":{},"subject":[],"published":{"date-parts":[[2012,6]]}}}